Exhaust nozzle for a gas turbine engine

Details Exhaust nozzle for a gas turbine engine Exhaust nozzle for a gas turbine engine

1987-01-20

1989-01-31

Kashnikow, Andres

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle with jacketed or hollow...

23926519, 23926539, 60230, 60266, F02K 112

Patent

active

048010871

ABSTRACT:
An exhaust nozzle for a gas turbine engine comprises a substantially tubular duct structure to which is mounted flow directing flaps for varying the throat area of the nozzle. The duct structure is progressively shaped and deformed as it extends in a downstream direction to provide straight upper and lower lips to which respective upper and lower flaps are pivotally attached for selectively vectoring the exhaust flow. The opposing sidewalls extend vertically within the duct structure and protrude therefrom between which the flaps and exhaust orifice is thereby defined within an essentially tubular duct.

REFERENCES:
patent: 2799989 (1957-07-01), Kappus
patent: 2831321 (1958-04-01), Laucher
patent: 3374954 (1968-03-01), Card
patent: 4375276 (1983-03-01), Konarski
patent: 4605169 (1986-08-01), Mayers
patent: 4641782 (1987-02-01), Woodward

Affiliated with

Also associated with

Rating

Exhaust nozzle for a gas turbine engine does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Exhaust nozzle for a gas turbine engine, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Exhaust nozzle for a gas turbine engine will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-174277